Thrust Profile (N)
1.35s Burn WindowEngineered by Cesaroni Technology, the 305H226-14A is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 305.0 Ns over a 1.35 second burn window.
With an average thrust of 225.6 N and a peak of 362.3 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
360g TotalDesign wings in your spreadsheet
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